Design and development[edit]

The aircraft fuselage is made from welded steel tubing, while the wings are constructed from aluminum sheet. Its 10.97 m (36.0 ft) span wing has an area of 15.44 m2 (166.2 sq ft) and mounts flaps. The standard engines used is the 150 to 160 hp (112 to 119 kW) Lycoming O-320four-stroke powerplant.[2]